JP5559792B2 - 重量が低減されたタービンエンジン用の固定ベーンアセンブリ、ならびに少なくとも一つのそうした固定ベーンアセンブリを具備してなるタービンエンジン - Google Patents

重量が低減されたタービンエンジン用の固定ベーンアセンブリ、ならびに少なくとも一つのそうした固定ベーンアセンブリを具備してなるタービンエンジン Download PDF

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Publication number
JP5559792B2
JP5559792B2 JP2011524356A JP2011524356A JP5559792B2 JP 5559792 B2 JP5559792 B2 JP 5559792B2 JP 2011524356 A JP2011524356 A JP 2011524356A JP 2011524356 A JP2011524356 A JP 2011524356A JP 5559792 B2 JP5559792 B2 JP 5559792B2
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Japan
Prior art keywords
vane assembly
casing
stationary vane
hole
pin
Prior art date
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JP2011524356A
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English (en)
Japanese (ja)
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JP2012500936A (ja
Inventor
ステファーヌ・ピエール・ギヨーム・ブランシャール
マチュー・ダコウスキ
ファブリス・マルセル・ノエル・ガラン
モーリス・ギー・ジュデ
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
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SNECMA SAS
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/28—Arrangement of seals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • F05B2260/301—Retaining bolts or nuts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP2011524356A 2008-08-26 2009-08-25 重量が低減されたタービンエンジン用の固定ベーンアセンブリ、ならびに少なくとも一つのそうした固定ベーンアセンブリを具備してなるタービンエンジン Active JP5559792B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0855732 2008-08-26
FR0855732A FR2935429B1 (fr) 2008-08-26 2008-08-26 Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe
PCT/EP2009/060929 WO2010023204A1 (fr) 2008-08-26 2009-08-25 Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe

Publications (2)

Publication Number Publication Date
JP2012500936A JP2012500936A (ja) 2012-01-12
JP5559792B2 true JP5559792B2 (ja) 2014-07-23

Family

ID=40521494

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011524356A Active JP5559792B2 (ja) 2008-08-26 2009-08-25 重量が低減されたタービンエンジン用の固定ベーンアセンブリ、ならびに少なくとも一つのそうした固定ベーンアセンブリを具備してなるタービンエンジン

Country Status (9)

Country Link
US (1) US8864458B2 (ru)
EP (1) EP2318666B1 (ru)
JP (1) JP5559792B2 (ru)
CN (1) CN102132010B (ru)
BR (1) BRPI0917801A2 (ru)
CA (1) CA2734289A1 (ru)
FR (1) FR2935429B1 (ru)
RU (1) RU2515694C2 (ru)
WO (1) WO2010023204A1 (ru)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2940350B1 (fr) 2008-12-23 2011-03-18 Snecma Roue mobile de turbomachine a aubes en materiau composite munie d'un anneau ressort.
FR2972483B1 (fr) 2011-03-07 2013-04-19 Snecma Carter de turbine comportant des moyens de fixation de secteurs d'anneau
FR2983247B1 (fr) * 2011-11-29 2014-12-26 Snecma Ensemble redresseur - carter intermediaire pour une turbomachine
FR2995021B1 (fr) * 2012-09-04 2017-08-25 Snecma Dispositif d'alimentation en air pour turbines de moteurs d'aeronefs
FR3009579B1 (fr) 2013-08-07 2015-09-25 Snecma Carter de turbine en deux materiaux
GB201315449D0 (en) 2013-08-30 2013-10-16 Rolls Royce Plc A flow detector arrangement
FR3034129B1 (fr) 2015-03-27 2019-05-17 Safran Aircraft Engines Aube mobile de turbine a conception amelioree pour turbomachine d'aeronef
FR3055656B1 (fr) * 2016-09-02 2018-08-31 Safran Aircraft Engines Turbine pour une turbomachine, telle par exemple qu'un turboreacteur
FR3064297B1 (fr) * 2017-03-23 2019-03-22 Safran Aircraft Engines Turbine pour une turbomachine, telle par exemple qu'un turboreacteur
LU100192B1 (fr) * 2017-05-04 2018-11-05 Carpyz Sas Procédé de construction de propulseurs ou de moteurs contenus dans un carter cylindrique
FR3096397B1 (fr) * 2019-05-21 2021-04-16 Safran Aircraft Engines Pion amovible sur distributeur de turbomachine
DE102020203840A1 (de) 2020-03-25 2021-09-30 MTU Aero Engines AG Gasturbinenbauteil

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE507205A (ru) * 1950-12-08
US4728255A (en) * 1985-02-25 1988-03-01 General Electric Company Removable stiffening disk
US4725199A (en) * 1985-12-23 1988-02-16 United Technologies Corporation Snap ring construction
FR2637321B1 (fr) * 1988-10-05 1990-11-30 Snecma Rotor de turbomachine muni d'un dispositif de fixation des aubes
US5211541A (en) * 1991-12-23 1993-05-18 General Electric Company Turbine support assembly including turbine heat shield and bolt retainer assembly
US5372476A (en) * 1993-06-18 1994-12-13 General Electric Company Turbine nozzle support assembly
US5503490A (en) * 1994-05-13 1996-04-02 United Technologies Corporation Thermal load relief ring for engine case
US5839878A (en) * 1996-09-30 1998-11-24 United Technologies Corporation Gas turbine stator vane
US6095750A (en) * 1998-12-21 2000-08-01 General Electric Company Turbine nozzle assembly
DE19962244A1 (de) * 1999-12-22 2001-06-28 Rolls Royce Deutschland Kühlluft-Führungssystem im Hochdruck-Turbinenabschnitt eines Gasturbinen Triebwerkes
US6447250B1 (en) * 2000-11-27 2002-09-10 General Electric Company Non-integral fan platform
US6761034B2 (en) * 2000-12-08 2004-07-13 General Electroc Company Structural cover for gas turbine engine bolted flanges
US6428272B1 (en) * 2000-12-22 2002-08-06 General Electric Company Bolted joint for rotor disks and method of reducing thermal gradients therein
RU2260700C2 (ru) * 2003-11-24 2005-09-20 Открытое акционерное общество "Авиадвигатель" Сопловой аппарат турбины газотурбинного двигателя
GB0424883D0 (en) * 2004-11-11 2004-12-15 Rolls Royce Plc Seal structure
US7341429B2 (en) * 2005-11-16 2008-03-11 General Electric Company Methods and apparatuses for cooling gas turbine engine rotor assemblies
FR2902843A1 (fr) 2006-06-23 2007-12-28 Snecma Sa Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine
FR2907499B1 (fr) * 2006-10-24 2011-12-23 Snecma Module de stator de distributeur de turbine a haute pression et turbomachine comportant ce module
US7578653B2 (en) * 2006-12-19 2009-08-25 General Electric Company Ovate band turbine stage

Also Published As

Publication number Publication date
EP2318666A1 (fr) 2011-05-11
RU2011111515A (ru) 2012-10-10
US8864458B2 (en) 2014-10-21
RU2515694C2 (ru) 2014-05-20
CN102132010A (zh) 2011-07-20
WO2010023204A1 (fr) 2010-03-04
BRPI0917801A2 (pt) 2016-03-01
EP2318666B1 (fr) 2013-07-31
FR2935429A1 (fr) 2010-03-05
CN102132010B (zh) 2014-04-16
CA2734289A1 (fr) 2010-03-04
FR2935429B1 (fr) 2011-11-25
JP2012500936A (ja) 2012-01-12
US20110206504A1 (en) 2011-08-25

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